View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66513U 26145.62702352 +.00000000 +00000-0 +12409-2 0 00007
2 66513 43.0025 276.3443 0002012 270.4325 89.6296 15.27595012 01
| Epoch (UTC): | 25 May 2026 15:02:54 |
| Eccentricity: | 0.0002012 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.3443° |
| argument of perigee: | 270.4325° |
| revolutions per day: | 15.27595012 |
| mean anomaly at epoch: | 89.6296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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